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RD-118


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RD-118 Part of RD-107 Glushko LOx/Kerosene rocket engine. In production. Update of RD-107, used in Soyuz ST launcher. Little performance change from RD-107, changes may mainly relate to use of all-Russian components. First flight 2001.

Status: In production. Number: 19 . Thrust: 999.60 kN (224,719 lbf). Specific impulse: 311 s. Specific impulse sea level: 245 s. Burn time: 300 s.

Chambers: 4. Oxidizer to Fuel Ratio: 2.39.

Country: Russia. Launch Vehicles: Soyuz-ST-B. Propellants: Lox/Kerosene. Stages: Soyuz ST-1. Agency: Glushko bureau. Bibliography: 318, 7498. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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